CN203954686U - A kind of X-type four axle model airplane skeleton and install bins thereof - Google Patents
A kind of X-type four axle model airplane skeleton and install bins thereof Download PDFInfo
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- CN203954686U CN203954686U CN201420383471.0U CN201420383471U CN203954686U CN 203954686 U CN203954686 U CN 203954686U CN 201420383471 U CN201420383471 U CN 201420383471U CN 203954686 U CN203954686 U CN 203954686U
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- crossbearer
- limited block
- plate
- external part
- installation sleeve
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Abstract
A kind of X-type four axle model airplane skeleton and install bins thereof, by upper skeleton plate, sending down the fishbone frame plate, crossbearer, crossbearer installation sleeve, pack up limited block, launch limited block, motor installation sleeve forms, it is characterized in that: described upper and lower frame board structure is identical, all be X-shaped, upper and lower frame board is connected and is a layer shape hollow structure by studs; Crossbearer installation sleeve, pack up limited block, launch limited block and be all arranged in layer shape hollow structure, crossbearer installation sleeve is connected with crossbearer, one end of crossbearer is provided with motor installation sleeve, packs up limited block, launches limited block and can carry out spacing to the position of packing up with launching of crossbearer respectively.The X-type four axle model airplane skeletons that the utility model provides, have simple in structure, lightweight, easily manufactured, keep in repair convenient, the easy feature such as folding, carrying when storing, do not take redundant space, strengthened model airplane fan customer experience.
Description
Technical field
The utility model relates to the structure field of model airplane skeleton, relates in particular to a kind of folding model airplane skeleton and install bin thereof.
Background technology
The kind of model airplane is a lot, and wherein most external styling is fixing not folding, need take a lot of spaces, carries and stores all inconveniences.Also having to adopt is designed to folding by the part-structure of model airplane (as wing, screw etc.), as patent CN201410055618, just wing, Design of Propeller become folding respectively with CN201220225932, this has saved space to a certain extent, but for X-type four axle model airplane structures, the skeleton forming because of fuselage and propeller bracket takes up space at most, only wing, Design of Propeller are become to folding, save space DeGrain.
Summary of the invention
The purpose of this utility model is to propose a kind of X-type four axle model airplane skeletons, have simple in structure, easily manufactured, keep in repair the features such as convenient, collapsible, carrying when storing, do not take redundant space, strengthen model airplane fan customer experience.
For achieving the above object, embodiment of the present utility model adopts following technical scheme:
A kind of X-type four axle model airplane skeletons that the utility model embodiment proposes, by upper skeleton plate, sending down the fishbone frame plate, crossbearer, crossbearer installation sleeve, motor installation sleeve, pack up limited block, expansion limited block forms, it is characterized in that: described upper skeleton plate, lower skeleton plate structure is identical, all be X-shaped, upper skeleton plate is along length direction bilateral symmetry, frame board in length direction stage casing is main framing plate, Liang Ge corner along the length direction both sides of main framing plate, be respectively equipped with a vertical external part, a parallel external part, at each vertical external part, be equipped with oblique angle external part with parallel external part place, vertical external part, parallel external part, oblique angle external part, main framing plate is machined forming of carbon fiber sectional material plate, at described vertical external part, be equipped with crossbearer installation sleeve installing hole with the junction of the junction of oblique angle external part, parallel external part and oblique angle external part, be separately installed with crossbearer installation sleeve, in the outside of each oblique angle external part, be provided with and launch limited block installing hole, in the outside of each vertical external part and parallel external part, be provided with and pack up limited block installing hole, and be separately installed with and launch limited block, pack up limited block, place, outer at upper skeleton plate, sending down the fishbone frame plate is provided with some upper and lower plates connecting holes, can upper skeleton plate, sending down the fishbone frame plate be connected and be a layer shape hollow structure by studs, described crossbearer is tubular type section bar, and its one end is connected with crossbearer installation sleeve, and the other end is installed with motor installation sleeve, described crossbearer installation sleeve is comprised of crossbearer installation sleeve installation end, crossbearer installation trepanning, crossbearer installation sleeve body, crossbearer installation sleeve installation end is provided with through hole, coordinate with the crossbearer installation sleeve installing hole at upper skeleton plate, by pin, crossbearer installation sleeve is arranged in the layer shape hollow structure of upper skeleton plate, sending down the fishbone frame plate formation, and form with it active link, crossbearer is installed trepanning and is fixedly connected with crossbearer, described expansion limited block, to pack up limited block structure identical, all with limited block installation end, spacing draw-in groove end, limited block installation end is provided with limited block installing hole, can be with expansion limited block installing hole on upper skeleton plate, pack up limited block installing hole and coordinate, and be bolted launching limited block, pack up limited block and be arranged on respectively in the layer shape hollow structure that upper and lower frame board forms.
Further, in order to reduce the aesthetics of weight and raising frame board, on upper skeleton plate, sending down the fishbone frame plate, be equipped with different special-shaped hole slot.
Further; in order to carry convenient and protection model airplane skeleton; also be provided with a kind of X-type corresponding with the utility model profile four axle model airplane skeleton install bins; skeleton install bin is put cavity, case body, annex by skeleton and is put cavity and form; what skeleton was put cavity is shaped as upper skeleton plate outline curve; it is corresponding with other accessory shape of fill that described annex is put the shape of cavity, for putting other accessory.
A kind of X-type four axle model airplane skeletons that the utility model provides, adopted the frame board that upper and lower double-layer structure is identical to be a layer shape hollow structure by Stud connection, crossbearer installation sleeve, pack up limited block, launch limited block and be all arranged in layer shape hollow structure, crossbearer installation sleeve is connected with crossbearer, one end of crossbearer is provided with motor installation sleeve, packs up limited block, launches limited block and can carry out spacing to the position of packing up with launching of crossbearer respectively.The X-type four axle model airplane skeletons that the utility model provides, have simple in structure, lightweight, easily manufactured, keep in repair convenient, the easy feature such as folding, carrying when storing, do not take redundant space, strengthened model airplane fan customer experience.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, accompanying drawing in the following describes is only embodiment more of the present utility model, for those of ordinary skills, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the front view of upper skeleton plate in the utility model;
Fig. 2 is the structural representation of crossbearer installation sleeve in the utility model;
Fig. 3 launches the structural representation of limited block in the utility model;
Fig. 4 be in the utility model crossbearer at the layout schematic diagram of upper and lower frame board;
Fig. 5 is the installation diagram front view that in the utility model, crossbearer is packed up in upper and lower frame board;
Fig. 6 is the installation diagram front view that in the utility model, crossbearer launches in upper and lower frame board;
Fig. 7 is the structural representation of model airplane skeleton install bin in the utility model;
Fig. 8 is the scheme of installation that the skeleton install bin of upper and lower frame board is installed in the utility model;
In figure: 1-upper skeleton plate; 2-crossbearer; 3-crossbearer installation sleeve; 4-pack up limited block; 5-expansion limited block; 6-motor installation sleeve; 7-skeleton install bin; 8-sending down the fishbone frame plate; 101-oblique angle external part; 102-expansion limited block installing hole; 103-crossbearer installation sleeve installing hole; 104-vertical external part; 105-pack up limited block installing hole; 106-main framing plate; 107-upper and lower plates connecting hole; 108-parallel external part; 109-special-shaped hole slot; 301-crossbearer installation sleeve installation end; 302-crossbearer is installed trepanning; 303-crossbearer installation sleeve body; 501-limited block installation end; 502-spacing draw-in groove end; 503-limited block installing hole; 701-skeleton is put cavity; 702-case body; 703-annex is put cavity.
The specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is only the utility model part embodiment, rather than whole embodiment.Embodiment based in the utility model, those of ordinary skills are not making the every other embodiment obtaining under creative work prerequisite, all belong to the scope of the utility model protection.
A kind of X-type four axle model airplane skeletons that the utility model embodiment proposes, as shown in Figures 1 to 6, by upper skeleton plate 1, sending down the fishbone frame plate 8, crossbearer 2, crossbearer installation sleeve 3, pack up limited block 4, launch limited block 5, motor installation sleeve 6 forms, it is characterized in that: described upper skeleton plate 1, sending down the fishbone frame plate 8 structures are identical, all be X-shaped, upper skeleton plate 1 is symmetrical along length direction, frame board in length direction stage casing is main framing plate 106, the Liang Ge corner along length direction both sides at main framing plate 106, be respectively equipped with a vertical external part 104, a parallel external part 108, at each vertical external part 104, be equipped with oblique angle external part 101 with parallel external part 108 places, vertical external part 104, parallel external part 108, oblique angle external part 101, main framing plate 106 is machined forming of carbon fiber sectional material plate, at described vertical external part 104, be equipped with crossbearer installation sleeve installing hole 103 with the junction of oblique angle external part 101, parallel external part 108 with the junction of oblique angle external part 101, be separately installed with crossbearer installation sleeve 3, in the outside of each oblique angle external part 101, be provided with and launch limited block installing hole 102, in the outside of each vertical external part 104 and parallel external part 108, be provided with and pack up limited block installing hole 105, and be separately installed with and launch limited block 5, pack up limited block 4, place, outer at upper skeleton plate 1, sending down the fishbone frame plate 8 is provided with some upper and lower plates connecting holes 107, can upper skeleton plate 1, sending down the fishbone frame plate 8 be connected to a layer shape hollow structure by studs, described crossbearer 2 is tubular type section bar, and its one end is connected with crossbearer installation sleeve 3, and the other end is installed with motor installation sleeve 6, described crossbearer installation sleeve 3 is comprised of crossbearer installation sleeve installation end 301, crossbearer installation trepanning 302, crossbearer installation sleeve body 303, crossbearer installation sleeve installation end 301 is provided with through hole, coordinate with the crossbearer installation sleeve installing hole 103 at upper skeleton plate 1, by pin, crossbearer installation sleeve 3 is arranged in the layer shape hollow structure of upper skeleton plate 1, sending down the fishbone frame plate 8 formations, and form with it active link, crossbearer is installed trepanning 302 and is fixedly connected with crossbearer 2, described pack up limited block 4, to launch limited block 5 structures identical, all with limited block installation end 501, spacing draw-in groove end 502, limited block installation end 501 is provided with limited block installing hole 503, can be with the expansion limited block installing hole 102 of upper skeleton plate 1, pack up limited block installing hole 105 and coordinate, be bolted packing up limited block 4, launch limited block 5 and be arranged on respectively in the layer shape hollow structure that upper skeleton plate 1, sending down the fishbone frame plate 8 form.
Further, the aesthetics for weight reduction and raising frame board is equipped with different special-shaped hole slot 109 on upper skeleton plate 1, sending down the fishbone frame plate 8.
Further; in order to carry convenient and protection model airplane skeleton; also be provided with a kind of X-type corresponding with model airplane skeleton four axle model airplane skeleton install bins 7; as shown in Figure 7 and Figure 8; it is put cavity 701, case body 702, annex by skeleton and puts cavity 703 and form; skeleton is put the outline curve that is shaped as upper skeleton plate 1 of cavity 701, and it is corresponding with other accessory shape of fill that described annex is put the shape of cavity 703, for putting other accessory.
The above; it is only the specific embodiment of the present utility model; but protection domain of the present utility model is not limited to this; anyly be familiar with those skilled in the art in the technical scope that the utility model discloses; can expect easily changing or replacing, within all should being encompassed in protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with the protection domain of described claim.
Claims (3)
1. X-type four axle model airplane skeletons, by upper skeleton plate (1), sending down the fishbone frame plate (8), crossbearer (2), crossbearer installation sleeve (3), pack up limited block (4), launch limited block (5), motor installation sleeve (6) forms, it is characterized in that: described upper skeleton plate (1), sending down the fishbone frame plate (8) structure is identical, all be X-shaped, upper skeleton plate (1) is along length direction bilateral symmetry, frame board in length direction stage casing is main framing plate (106), Liang Ge corner in the length direction both sides along main framing plate (106), be respectively equipped with a vertical external part (104), a parallel external part (108), at each vertical external part (104), locate to be equipped with oblique angle external part (101) with parallel external part (108), vertical external part (104), parallel external part (108), oblique angle external part (101), main framing plate (106) is machined forming of carbon fiber sectional material plate, at described vertical external part 104, be equipped with crossbearer installation sleeve installing hole (103) with the junction of oblique angle external part (101), parallel external part (108) with the junction of oblique angle external part (101), be separately installed with crossbearer installation sleeve (3), in the outside of each oblique angle external part (101), be provided with and launch limited block installing hole (102), in the outside of each vertical external part (104) and parallel external part (108), be provided with and pack up limited block installing hole (105), and be separately installed with and launch limited block (5), pack up limited block (4), place, outer at upper skeleton plate (1), sending down the fishbone frame plate (8) is provided with some upper and lower plates connecting holes (107), can upper skeleton plate (1), sending down the fishbone frame plate (8) be connected and be a layer shape hollow structure by studs, described crossbearer (2) is tubular type section bar, and its one end is connected with crossbearer installation sleeve (3), and the other end is installed with motor installation sleeve (6), described crossbearer installation sleeve (3) is comprised of crossbearer installation sleeve installation end (301), crossbearer installation trepanning (302), crossbearer installation sleeve body (303), crossbearer installation sleeve installation end (301) is provided with through hole, coordinate with the crossbearer installation sleeve installing hole (103) at upper skeleton plate (1), by pin, crossbearer installation sleeve body (303) is arranged in the layer shape hollow structure of upper skeleton plate (1), sending down the fishbone frame plate (8) formation, and form with it active link, crossbearer is installed trepanning (302) and is fixedly connected with crossbearer (2), described pack up limited block (4), to launch limited block (5) structure identical, all with limited block installation end (501), spacing draw-in groove end (502), limited block installation end (501) is provided with limited block installing hole (503), can be with the expansion limited block installing hole (102) of upper skeleton plate (1), pack up limited block installing hole (105) and coordinate, and be bolted packing up limited block (4), launch limited block (5) and be arranged on respectively in the layer shape hollow structure that upper skeleton plate (1), sending down the fishbone frame plate (8) form.
2. a kind of X-type four axle model airplane skeletons according to claim 1, is characterized in that: on described upper skeleton plate (1) and sending down the fishbone frame plate (8), be also respectively equipped with different special-shaped hole slot (109).
3. X-type four axle model airplane skeleton install bins, by skeleton, putting cavity (701), case body (702), annex puts cavity (703) and forms, it is characterized in that: described skeleton is put the outline curve that is shaped as upper skeleton plate (1) of cavity (701), the shape that described annex is put cavity (703) with to fill other accessory shape corresponding.
Priority Applications (1)
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CN201420383471.0U CN203954686U (en) | 2014-07-12 | 2014-07-12 | A kind of X-type four axle model airplane skeleton and install bins thereof |
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CN201420383471.0U CN203954686U (en) | 2014-07-12 | 2014-07-12 | A kind of X-type four axle model airplane skeleton and install bins thereof |
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CN203954686U true CN203954686U (en) | 2014-11-26 |
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CN201420383471.0U Expired - Fee Related CN203954686U (en) | 2014-07-12 | 2014-07-12 | A kind of X-type four axle model airplane skeleton and install bins thereof |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105797392A (en) * | 2014-12-27 | 2016-07-27 | 张向东 | A foldable tilted aeromodel support component |
-
2014
- 2014-07-12 CN CN201420383471.0U patent/CN203954686U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105797392A (en) * | 2014-12-27 | 2016-07-27 | 张向东 | A foldable tilted aeromodel support component |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141126 Termination date: 20150712 |
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EXPY | Termination of patent right or utility model |